FR2964086B1 - Procede d'optimisation du rendement energetique global d'un aeronef et groupe de puissance principal de mise en oeuvre - Google Patents

Procede d'optimisation du rendement energetique global d'un aeronef et groupe de puissance principal de mise en oeuvre

Info

Publication number
FR2964086B1
FR2964086B1 FR1056761A FR1056761A FR2964086B1 FR 2964086 B1 FR2964086 B1 FR 2964086B1 FR 1056761 A FR1056761 A FR 1056761A FR 1056761 A FR1056761 A FR 1056761A FR 2964086 B1 FR2964086 B1 FR 2964086B1
Authority
FR
France
Prior art keywords
aircraft
implementation
main power
power package
energetic efficiency
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR1056761A
Other languages
English (en)
French (fr)
Other versions
FR2964086A1 (fr
Inventor
Jean Michel Haillot
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Helicopter Engines SAS
Original Assignee
Turbomeca SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to FR1056761A priority Critical patent/FR2964086B1/fr
Application filed by Turbomeca SA filed Critical Turbomeca SA
Priority to ES11761653.2T priority patent/ES2618904T3/es
Priority to US13/817,183 priority patent/US8868262B2/en
Priority to KR1020137005235A priority patent/KR101860164B1/ko
Priority to CN201180040506.XA priority patent/CN103108805B/zh
Priority to CA2808180A priority patent/CA2808180C/fr
Priority to RU2013107596/11A priority patent/RU2585394C2/ru
Priority to EP11761653.2A priority patent/EP2609012B1/de
Priority to PCT/FR2011/051943 priority patent/WO2012025687A2/fr
Priority to PL11761653T priority patent/PL2609012T3/pl
Priority to JP2013525337A priority patent/JP5873493B2/ja
Publication of FR2964086A1 publication Critical patent/FR2964086A1/fr
Application granted granted Critical
Publication of FR2964086B1 publication Critical patent/FR2964086B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0611—Environmental Control Systems combined with auxiliary power units (APU's)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/50—Application for auxiliary power units (APU's)
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/50—On board measures aiming to increase energy efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
  • Fluid-Pressure Circuits (AREA)
FR1056761A 2010-08-25 2010-08-25 Procede d'optimisation du rendement energetique global d'un aeronef et groupe de puissance principal de mise en oeuvre Expired - Fee Related FR2964086B1 (fr)

Priority Applications (11)

Application Number Priority Date Filing Date Title
FR1056761A FR2964086B1 (fr) 2010-08-25 2010-08-25 Procede d'optimisation du rendement energetique global d'un aeronef et groupe de puissance principal de mise en oeuvre
PCT/FR2011/051943 WO2012025687A2 (fr) 2010-08-25 2011-08-23 Procédé d'optimisation du rendement énergétique global d'un aéronef et groupe de puissance principal de mise en oeuvre
KR1020137005235A KR101860164B1 (ko) 2010-08-25 2011-08-23 항공기의 전체 에너지 효율 최적화 및 이를 실현하기 위한 메인 동력 패키지
CN201180040506.XA CN103108805B (zh) 2010-08-25 2011-08-23 优化飞机总能量效率的方法，和实施这种方法的主动力装置
CA2808180A CA2808180C (fr) 2010-08-25 2011-08-23 Procede d'optimisation du rendement energetique global d'un aeronef et groupe de puissance principal de mise en oeuvre
RU2013107596/11A RU2585394C2 (ru) 2010-08-25 2011-08-23 Способ оптимизации общей энергетической эффективности летательного аппарата и основная силовая группа для осуществления
ES11761653.2T ES2618904T3 (es) 2010-08-25 2011-08-23 Procedimiento de optimización del rendimiento energético global de una aeronave y grupo de potencia principal de puesta en práctica
US13/817,183 US8868262B2 (en) 2010-08-25 2011-08-23 Method for optimizing the overall energy efficiency of an aircraft, and main power package for implementing same
PL11761653T PL2609012T3 (pl) 2010-08-25 2011-08-23 Sposób optymalizacji ogólnej wydajności energii statku powietrznego i główny zespół mocy do realizacji takiego sposobu
JP2013525337A JP5873493B2 (ja) 2010-08-25 2011-08-23 航空機の全エネルギー効率を最適化する方法、およびそれを実施するためのメインパワーパッケージ
EP11761653.2A EP2609012B1 (de) 2010-08-25 2011-08-23 Verfahren zur optimierung des gesamtenergetischen nutzeffekts eines flugzeugs und diesbezügliche hauptmotorbaugruppe

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1056761A FR2964086B1 (fr) 2010-08-25 2010-08-25 Procede d'optimisation du rendement energetique global d'un aeronef et groupe de puissance principal de mise en oeuvre

Publications (2)

Publication Number Publication Date
FR2964086A1 FR2964086A1 (fr) 2012-03-02
FR2964086B1 true FR2964086B1 (fr) 2013-06-14

Family

ID=43799500

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1056761A Expired - Fee Related FR2964086B1 (fr) 2010-08-25 2010-08-25 Procede d'optimisation du rendement energetique global d'un aeronef et groupe de puissance principal de mise en oeuvre

Country Status (11)

Country Link
US (1) US8868262B2 (de)
EP (1) EP2609012B1 (de)
JP (1) JP5873493B2 (de)
KR (1) KR101860164B1 (de)
CN (1) CN103108805B (de)
CA (1) CA2808180C (de)
ES (1) ES2618904T3 (de)
FR (1) FR2964086B1 (de)
PL (1) PL2609012T3 (de)
RU (1) RU2585394C2 (de)
WO (1) WO2012025687A2 (de)

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GB201219922D0 (en) * 2012-11-06 2012-12-19 Rolls Royce Plc Method of controlling an aircraft electrical power generation system
FR3001442B1 (fr) * 2013-01-29 2016-05-20 Microturbo Architecture de fourniture de puissance electrique de secours amelioree dans un aeronef
US10266276B2 (en) * 2013-03-14 2019-04-23 Textron Innovations, Inc. Integrated auxiliary power unit, starter-generator-motor, and vapor cycle cooling system for an aircraft
WO2014143187A1 (en) * 2013-03-15 2014-09-18 Michael Armstrong Lifing and performance optimization limit management for turbine engine
US10569892B2 (en) 2013-05-06 2020-02-25 Sikorsky Aircraft Corporation Supplemental power for reduction of prime mover
FR3019358B1 (fr) * 2014-03-27 2016-03-18 Turbomeca Procede de gestion globale optimisee d'un reseau energetique d'un aeronef et dispositif correspondant
US9354621B2 (en) 2014-06-16 2016-05-31 General Electric Company Systems and methods for control of an adaptive-cycle engine with power-thermal management system
EP3095703B1 (de) * 2015-05-11 2019-07-03 United Technologies Corporation Umgebungskühlsysteme für flugzeuge
US10240521B2 (en) 2015-08-07 2019-03-26 Pratt & Whitney Canada Corp. Auxiliary power unit with variable speed ratio
JP5973096B1 (ja) * 2016-01-14 2016-08-23 三菱日立パワーシステムズ株式会社 プラント分析装置、プラント分析方法、およびプログラム
EP3254970B1 (de) * 2016-05-26 2020-04-29 Hamilton Sundstrand Corporation Klimaregelungssystem mit einem abströmungswärmetauscher
US11511867B2 (en) 2016-05-26 2022-11-29 Hamilton Sundstrand Corporation Mixing ram and bleed air in a dual entry turbine system
US11506121B2 (en) 2016-05-26 2022-11-22 Hamilton Sundstrand Corporation Multiple nozzle configurations for a turbine of an environmental control system
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US10919638B2 (en) 2016-05-31 2021-02-16 The Boeing Company Aircraft cabin pressurization energy harvesting
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US11214380B2 (en) 2017-05-31 2022-01-04 General Electric Company Intelligent mission thermal management system
US20190002117A1 (en) * 2017-06-30 2019-01-03 General Electric Company Propulsion system for an aircraft
US11061414B2 (en) 2017-12-20 2021-07-13 General Electric Company Fleet mission advisor
CN108520108B (zh) * 2018-03-19 2022-02-18 中国海洋石油集团有限公司 一种基于温度场分析的浮式液化天然气装置液舱优化方法
US11273917B2 (en) * 2018-05-29 2022-03-15 Honeywell International Inc. Cabin discharge air management system and method for auxiliary power unit
WO2020079892A1 (ja) * 2018-10-18 2020-04-23 株式会社Ihi 航空機用エネルギ回収装置
US10839698B1 (en) * 2019-06-18 2020-11-17 Honeywell International Inc. Methods and systems for depicting an energy state of a vehicle
CN113022863B (zh) * 2021-04-19 2022-07-22 中国航发湖南动力机械研究所 辅助动力装置及辅助动力装置的排气控制方法
CN114954964B (zh) * 2022-06-08 2024-04-16 中国航空发动机研究院 一种喷管装置及航空发动机
CN114872908B (zh) * 2022-06-08 2024-03-26 中国航空发动机研究院 一种喷管装置及航空发动机
US12012217B2 (en) * 2022-08-22 2024-06-18 Gulfstream Aerospace Corporation Auxiliary power unit air inlet door with specified acoustic reflecting and/or diffusing characteristics

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Also Published As

Publication number Publication date
CA2808180C (fr) 2018-06-26
WO2012025687A2 (fr) 2012-03-01
CN103108805A (zh) 2013-05-15
CN103108805B (zh) 2016-02-10
EP2609012B1 (de) 2017-02-22
KR101860164B1 (ko) 2018-06-27
KR20130105612A (ko) 2013-09-25
RU2013107596A (ru) 2014-09-27
EP2609012A2 (de) 2013-07-03
WO2012025687A3 (fr) 2012-04-19
US20130151039A1 (en) 2013-06-13
PL2609012T3 (pl) 2017-08-31
RU2585394C2 (ru) 2016-05-27
ES2618904T3 (es) 2017-06-22
CA2808180A1 (fr) 2012-03-01
US8868262B2 (en) 2014-10-21
JP2013538153A (ja) 2013-10-10
FR2964086A1 (fr) 2012-03-02
JP5873493B2 (ja) 2016-03-01

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